EP1795628A1 - Plaquette de coupe pour fraise d'acier - Google Patents
Plaquette de coupe pour fraise d'acier Download PDFInfo
- Publication number
- EP1795628A1 EP1795628A1 EP06124268A EP06124268A EP1795628A1 EP 1795628 A1 EP1795628 A1 EP 1795628A1 EP 06124268 A EP06124268 A EP 06124268A EP 06124268 A EP06124268 A EP 06124268A EP 1795628 A1 EP1795628 A1 EP 1795628A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- coating
- range
- milling
- tooth
- insert
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000003801 milling Methods 0.000 title claims abstract description 14
- 229910000831 Steel Inorganic materials 0.000 title abstract description 6
- 239000010959 steel Substances 0.000 title abstract description 6
- 238000000576 coating method Methods 0.000 claims abstract description 35
- 239000011248 coating agent Substances 0.000 claims abstract description 33
- 238000005520 cutting process Methods 0.000 claims abstract description 24
- 239000000758 substrate Substances 0.000 claims abstract description 15
- 239000000203 mixture Substances 0.000 claims abstract description 10
- 229910001220 stainless steel Inorganic materials 0.000 claims abstract description 4
- 239000000126 substance Substances 0.000 claims abstract 2
- 230000003252 repetitive effect Effects 0.000 claims description 5
- 230000008020 evaporation Effects 0.000 claims description 4
- 238000001704 evaporation Methods 0.000 claims description 4
- 229910052751 metal Inorganic materials 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 229910000851 Alloy steel Inorganic materials 0.000 claims description 3
- 229910010038 TiAl Inorganic materials 0.000 claims description 2
- 229910045601 alloy Inorganic materials 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 239000012298 atmosphere Substances 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 claims description 2
- 238000000151 deposition Methods 0.000 claims 2
- 239000000463 material Substances 0.000 abstract description 6
- 239000010935 stainless steel Substances 0.000 abstract description 2
- 239000010936 titanium Substances 0.000 abstract 4
- -1 HRSA Substances 0.000 abstract 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 abstract 1
- 239000007787 solid Substances 0.000 abstract 1
- 229910052719 titanium Inorganic materials 0.000 abstract 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 abstract 1
- 239000011230 binding agent Substances 0.000 description 4
- 241000446313 Lamella Species 0.000 description 3
- 238000005336 cracking Methods 0.000 description 3
- 238000004626 scanning electron microscopy Methods 0.000 description 3
- 229910001315 Tool steel Inorganic materials 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 239000002826 coolant Substances 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 239000000839 emulsion Substances 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000003112 inhibitor Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 239000012299 nitrogen atmosphere Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 230000009528 severe injury Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000004227 thermal cracking Methods 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B27/00—Tools for turning or boring machines; Tools of a similar kind in general; Accessories therefor
- B23B27/14—Cutting tools of which the bits or tips or cutting inserts are of special material
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
- C23C30/005—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process on hard metal substrates
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C29/00—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
- C22C29/02—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides
- C22C29/06—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds
- C22C29/08—Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on carbides or carbonitrides based on carbides, but not containing other metal compounds based on tungsten carbide
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0617—AIII BV compounds, where A is Al, Ga, In or Tl and B is N, P, As, Sb or Bi
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0641—Nitrides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/24—Vacuum evaporation
- C23C14/32—Vacuum evaporation by explosion; by evaporation and subsequent ionisation of the vapours, e.g. ion-plating
- C23C14/325—Electric arc evaporation
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/3464—Sputtering using more than one target
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T407/00—Cutters, for shaping
- Y10T407/27—Cutters, for shaping comprising tool of specific chemical composition
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/2495—Thickness [relative or absolute]
- Y10T428/24967—Absolute thicknesses specified
- Y10T428/24975—No layer or component greater than 5 mils thick
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
- Y10T428/265—1 mil or less
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
Definitions
- the present invention pertains to a coated cemented carbide insert for machining of steels or stainless steel when a high wear resistance combined with a high edge toughness are required.
- the thermal load on the insert will vary over time, something that often induces thermal tension and subsequently may generate thermally induced cracks in the coatings. This is especially a concern with cooled/ wet operations where the thermal variations are more pronounced than in dry operations.
- a common wear mechanism in milling is cracking, followed by chipping or small fragments of the cutting edge loosening from the rest of the substrate. Increasing the edge toughness is thus of great importance to increase tool lifetime.
- One possible solution to decrease the risk of thermal cracking -as well as cracking for various other reasons- is to use a multilayered coating.
- the multilayered coating is expected to act as a crack inhibitor as an initial crack going down the coating may be redirected at any sublayer interface.
- Another benefit of multilayer coatings is expected to show up when hard, wear resistant layers are interlaid with a softer sublayer. The softer layer may be able to absorb shocks and thus inhibit cracks from penetrating the whole coating.
- WO 98/48072 relates to a cutting tool comprising a body of sintered cemented carbide, ceramic or high speed steel on which at least on the functional parts of the surface of the body, a thin, adherent, hard and wear resistant coating is applied.
- the coating comprises a laminar, multilayered structure of refractory compounds in polycrystalline, non-repetitive form MX+NX+MX+NX... where the alternating layers MX and NX are composed of metal nitrides or metal carbides.
- the sequence of individual layer thicknesses is essentially aperiodic throughout the entire multilayered structure.
- Figure 1 shows a scanning electron microscopy (SEM) picture of the coating with all the individual multilayers.
- Figure 2 shows a SEM picture of a detail of the coating where the individual layers are measured, and where the essentially aperiodic nature of the layer structure is evident.
- SEM scanning electron microscopy
- a coated cutting tool insert is provided of a cemented carbide body with a composition of 8-11 wt-% Co, preferably 9.5-10.5 wt-% Co, most preferably 9.9-10.1 wt-% Co, 0.1-0.5 wt-% Cr, preferably 0.38-0.40 wt-% Cr and balance WC.
- the cemented carbide body may also contain smaller amounts of other elements, on a level corresponding to a technical impurity.
- the coercivity is in the range 18-22 kA/m, preferably 19-21 kA/m, most preferably 19.8-20.2 kA/m.
- the cobalt binder phase is alloyed with a certain amount of W and Cr giving the invented cemented carbide cutting insert its desired properties.
- the CW-ratio varies between 1 and about 0.75 dependent on the degree of alloying of the binder phase.
- the cemented carbide body has a CW-ratio in the range of 0.78-0.90, preferably within 0.80-0.89, and most preferably within 0.83-0.87.
- the cemented carbide may also contain small amounts, ⁇ 1 volume %, of ⁇ -phase (M 6 C), without any detrimental effects. From the specified CW-ratios ( ⁇ 1) it also follows that no free graphite is allowed in the cemented carbide body according to the present invention.
- the insert according to the present invention is provided with an aperiodic TiA1N multilayer consisting of a binary A+B+A+B+... structure with thin alternating sublayers A and B being repeated throughout the entire coating.
- One sequence of a sublayer A+B is here denoted a lamella. Due to the aperiodic nature of the coating, the thickness of each lamella will vary but in average the lamella thickness is within 30-300 nm, preferably 60-120 nm.
- the sublayer A comprises Al x Ti 1-x N, where x is 0.40-0.7, preferably 0.5-0.67.
- Layer B comprises of Ti y Al 1-y N, where y is 0.6-1, preferably 0.75-1.
- the stoichiometry for the whole coating as measured by e.g., microprobe or EDS, is within the interval Ti z Al 1-z N, z: 0.40-0.7, preferably 0.45-0.6.
- the total thickness of the multilayered coating is 0.5 ⁇ m to 15 ⁇ m, preferably 1 ⁇ m to 10 ⁇ m, more preferably 1-5 ⁇ m on the rake side and 2-8 ⁇ m on the flank side.
- there is an outer Ti b Al 1-b N layer, b 0.8-0.9, preferably 0.82-0.85, has sufficient thickness to give a visible, homogenous bronze-coloured look, preferably 0.1-1 ⁇ m thick.
- the present invention also relates to a method of making a cutting insert comprising a cemented carbide substrate and a coating.
- Onto this substrate is deposited a coating comprising a laminar, multilayered structure of A+B+A+B+...
- the total thickness of the multilayered coating is 0.5 ⁇ m to 15 ⁇ m, preferably 1 ⁇ m to 10 ⁇ m, more preferably 1-5 ⁇ m on the rake side and 2-8 ⁇ m on the flank side.
- the coating is deposited using cathodic arc evaporation using two or three pairs of arc sources consisting of pure Ti and/or TiAl alloy(s), in an N 2 or mixed N 2 +Ar gas atmosphere.
- an outer Ti b Al 1-b N layer, b 0.8-0.9, preferably 0.82-0.85, of sufficient thickness to give a visible, homogenous bronze-coloured look, preferably 0.1-1 ⁇ m thick, is deposited.
- the present invention also relates to the use of a cutting tool insert according to above in milling steel alloys and stainless steels, preferably under dry conditions, with cutting speeds and feed rates according to following table:
- Aperiodic multilayers were deposited by cathodic arc evaporation on cemented carbide milling inserts with a composition of 10 wt-% Co, 0.4 wt-% Cr and balance WC, and with a coercivity value of 20.2 kA/m and an CW-ratio of 0.85 as measured in the F ⁇ RSTER KOERZIMAT CS 1.096 from Foerster Instruments Inc.
- the multilayers were deposited from one pair of Ti 84 Al 16 targets and two pairs of Ti 33 Al 67 targets with the inserts mounted on a 3-fold rotating substrate table arranged in order to obtain the aperiodic structure.
- the arc evaporation was performed in a N 2 atmosphere.
- the total coating thickness was in the range 2-9 ⁇ m, varying from batch to batch, from insert to insert, and over the insert surface.
- the coating consisted of a binary A+B+A+B+... aperiodic multilayer, i.e. layers with a non-repetitive thickness, but with an average A+B layer thickness of 60-120 nm.
- the insert was coated with a final outer layer of Ti 84 Al 16 N to produce a bronze colour.
- the coating had an average composition Ti z Al 1-z N lying between the composition of the two sublayers A and B. This average composition was measured in a micro-probe at the centre of the flank side. A composition corresponding to Ti 0.5 Al 0.5 N was obtained.
- Inserts with a geometry R300-1648M-PH and with the same substrate composition and the same coating as those in Example 1 were tested and compared to Reference A with a homogenous Ti 33 Al 67 N layer of the same thickness deposited on inserts from the same substrate batch.
- the work material in this case was a tool steel with a hardness of 48 HRC.
- Inserts from Example 1 were tested and compared to a Reference A as well as Reference B.
- the geometry was in all cases R390-11T0308M-PM.
- the work material was an alloyed steel with a hardness of 220 HB.
- Reference B could machine 16 components, Reference A 24 components and the inserts from Example 1 could machine 40 components.
- the decisive difference in wear type for increasing the tool life was less chipping in edge line.
- Inserts from Example 1 were tested and compared to a Reference A as well as Reference B.
- the geometry were in all cases CM245-12T3 E-PL.
- the work material was an austenitic stainless steel.
- the inserts from Example 1 lasted 6 meters, Reference A lasted 3.5 meters and Reference B lasted 3 meters.
- the multilayer inserts from Example 1 clearly outperforms the other variants.
- the decisive difference in wear type for increasing the tool life was better edge line toughness (no cracks, no edge breakdown).
- Inserts from Example 1 were tested and compared to a Reference C according to Example 1 in patent application WO 01/16389 .
- the geometry was R210-140512M-PM in all cases.
- the work material was a tool steel with a hardness of 45 HRC.
- the inserts from Example 1 lasted 34 minutes whereas Reference C as best result achieved 14 minutes.
- the decisive difference in wear type for increasing the tool life was better notch wear resistance.
- the insert according to the invention is able to withstand all wear types better than other tested inserts, showing a more predictable edge line behaviour and being more reliable in unstable conditions. It allows an increase in cutting data.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
- Physical Vapour Deposition (AREA)
- Gear Processing (AREA)
- Milling Processes (AREA)
- Chemically Coating (AREA)
- Magnetic Heads (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0502694A SE529838C2 (sv) | 2005-12-08 | 2005-12-08 | Belagt hårdmetallskär, sätt att framställa detta samt dess användning för fräsning i stål |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1795628A1 true EP1795628A1 (fr) | 2007-06-13 |
EP1795628B1 EP1795628B1 (fr) | 2010-05-26 |
Family
ID=37575145
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06124268A Active EP1795628B1 (fr) | 2005-12-08 | 2006-11-17 | Plaquette de coupe pour fraise d'acier |
Country Status (9)
Country | Link |
---|---|
US (1) | US7727621B2 (fr) |
EP (1) | EP1795628B1 (fr) |
JP (1) | JP2007196365A (fr) |
KR (1) | KR101333559B1 (fr) |
CN (1) | CN1978192B (fr) |
AT (1) | ATE469251T1 (fr) |
DE (1) | DE602006014491D1 (fr) |
IL (1) | IL179577A0 (fr) |
SE (1) | SE529838C2 (fr) |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1900849A1 (fr) * | 2006-08-28 | 2008-03-19 | Sandvik Intellectual Property AB | Insertions de carbure métallique pour le fraisage d'alliages à base de Fe de roche à dureté HRC > 45 |
EP2011894A1 (fr) * | 2007-06-01 | 2009-01-07 | Sandvik Intellectual Property AB | Inserts de carbure métallique pour des rainurages, des séparations et de filetage |
WO2009031958A1 (fr) * | 2007-09-05 | 2009-03-12 | Sandvik Intellectual Property Ab | Foret enduit et procédé de fabrication associé |
EP2036997A1 (fr) * | 2007-06-01 | 2009-03-18 | Sandvik Intellectual Property AB | Inserts d'outils de découpe à carbure cimentée revêtue |
EP2039803A1 (fr) * | 2007-08-24 | 2009-03-25 | SECO TOOLS AB (publ) | Outil de coupe revêtu pour le tournage de superalliages résistant à la chaleur |
WO2009070109A1 (fr) * | 2007-11-28 | 2009-06-04 | Sandvik Intellectual Property Ab | Inserts de carbure cémentés revêtus pour fraisage d'engrenage dans des pièces coulées en acier à faible teneur en carbone |
WO2009070111A1 (fr) * | 2007-11-28 | 2009-06-04 | Sandvik Intellectual Property Ab | Inserts de carbure cémenté revêtus pour fraisage d'ébauche d'engrenages |
WO2009079184A3 (fr) * | 2007-12-14 | 2009-09-17 | Kennametal Inc. | Article revêtu à architecture de revêtement à nanocouches |
US7938878B2 (en) | 2007-06-01 | 2011-05-10 | Sandvik Intellectual Property Ab | Fine grained cemented carbide with refined structure |
US7976607B2 (en) | 2006-06-15 | 2011-07-12 | Sandvik Intellectual Property Ab | Cemented carbide with refined structure |
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US7976607B2 (en) | 2006-06-15 | 2011-07-12 | Sandvik Intellectual Property Ab | Cemented carbide with refined structure |
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WO2009079184A3 (fr) * | 2007-12-14 | 2009-09-17 | Kennametal Inc. | Article revêtu à architecture de revêtement à nanocouches |
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WO2013134796A1 (fr) * | 2012-03-14 | 2013-09-19 | Boehlerit Gmbh & Co.Kg. | Corps revêtu et procédé pour revêtir un corps |
AT516062A4 (de) * | 2015-01-15 | 2016-02-15 | Boehlerit Gmbh & Co Kg | Verfahren zum Beschichten eines Gegenstandes und damit hergestellte Beschichtung |
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US10597776B2 (en) | 2015-01-15 | 2020-03-24 | Boehlerit Gmbh & Co. Kg. | Process for coating an article and coating produced thereby |
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CN111331963B (zh) * | 2020-03-27 | 2024-01-05 | 嘉兴吉森科技有限公司 | 一种多层复合钢及多层复合钢刀具的制作方法 |
Also Published As
Publication number | Publication date |
---|---|
CN1978192B (zh) | 2012-09-05 |
SE0502694L (sv) | 2007-06-09 |
KR101333559B1 (ko) | 2013-11-27 |
CN1978192A (zh) | 2007-06-13 |
KR20070061456A (ko) | 2007-06-13 |
US7727621B2 (en) | 2010-06-01 |
US20070141346A1 (en) | 2007-06-21 |
ATE469251T1 (de) | 2010-06-15 |
SE529838C2 (sv) | 2007-12-04 |
IL179577A0 (en) | 2007-08-19 |
JP2007196365A (ja) | 2007-08-09 |
EP1795628B1 (fr) | 2010-05-26 |
DE602006014491D1 (de) | 2010-07-08 |
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